US20100313677A1

US20100313677A1 - Strain Gauge Rosette for Internal Stress Measurement

Info

Publication number: US20100313677A1
Application number: US12/744,189
Authority: US
Inventors: Sebastian Klein; Thomas Kleckers
Original assignee: Individual
Current assignee: Hottinger Bruel and Kjaer GmbH
Priority date: 2007-11-23
Filing date: 2008-11-24
Publication date: 2010-12-16
Also published as: CN101965506A; EP2238420A1; DE102007056443B3; US8210055B2; EP2238420B1; JP2011504589A; JP5237383B2; WO2009065615A1

Abstract

The invention relates to a strain gage rosette for internal stress measurement on workpieces according to the bore hole method, which comprises at least three measuring grids 3, 4, 5 within an angular range of 0-<180° at equal spacing and in different directions radially about a centering mark 2. The invention is characterized in that, to each one of the at least three measuring grids 3, 4, 5 there is allocated respectively a similar measuring grid 6, 7, 8, that is lying oppositely and oriented in the same direction. In that regard, all measuring grids 3, 4, 5, 6, 7, 8, 16, 17 have the same radial spacing to the centering mark 2. Whereby the oppositely lying measuring grid pairs 3, 8; 4, 7; 5, 6; 16, 17 of one strain direction circuit-connected or coupled with one another such that the measurement signals thereof are averaged.

Description

The invention relates to a strain gage rosette for internal stress measurement on workpieces according to the bore hole method according to the preamble of the patent claims 1 and 10.
For certain workpieces or structural components it is often necessary to determine if internal stresses are present therein, and what magnitude and direction these comprise. In that regard, the term internal stresses means stresses in a structural component that are effective without external mechanical loading and that are subject to a spatially homogeneous and temporally constant temperature field.
For measuring such internal stresses, there are various different testing methods with which the internal stress condition on the surface and in the interior of the material can be determined. In the range near the surface up to a depth of several millimeters, the bore hole method is often utilized. Thereby, a hole is bored at a certain location of the structural component at which the internal stresses are to be determined, wherein the diameter and the bore depth of the hole is based on the test sample thickness. Through this bore hole, a portion of the internal stresses present in the material is released, whereby measurable deformations arise in the vicinity of the bore hole rim.
By measuring these deformations in the region of the bore hole, a conclusion can then be reached about the effective internal stresses. For that, the strains in three different directions must be determined, for example by applying three strain gages that are grouped around the bore hole. In this method, however, only relatively small strain gages can be used, because the substantial analogy between the differential strain and the triggered internal stress portions exists only in the direct vicinity of the bore hole.
Such a method and a strain gage rosette used therefor is known from the DE-OS 25 58 768. Therein, the strain gage rosette consists of a carrier film on which three measuring grids are arranged at the angular positions of 0°, 45° and 90° around a central middle point or center point. In the internal stress measurement according to the bore hole method, the difficulty is that the workpiece is to be bored exactly in the middle of the glued-on rosette. Namely, with a bore hole that is not centrally applied, the strain measuring grids, which are then arranged at different radial distance, detect a spacing distance dependent strain, which then lead to measurement errors. Therefore, the strain gage rosette is glued-on with its center point exactly centered on a circuit board, whereby a centering bushing is soldered-on in the center of the circuit board. In that regard, a central bore hole is provided in the centering bushing, and a centering pin is inserted in the central bore hole. The strain gage rosette is then glued onto the workpiece to be tested.
For the exact introduction of the bore hole, then a special drilling or boring apparatus of a U-shaped metal bail with a drill or borer guide is arranged over the strain gage rosette, and is applied or set-on exactly centered to the strain gage rosette by a centering pin that is inserted in the centering bushing. Then, after the centering, the centering pin is removed out of the drilling or boring apparatus, and the shaft of a drilling or boring machine is inserted into the drilling or boring apparatus, in order to introduce into the workpiece a very exact central bore hole between the glued-on measuring grids. The strains that are thereby triggered during the drilling or boring process are then converted into electrical signals by the is strain gage grids, and then the internal stresses are calculable from the electrical signals. Because a substantial analogy between the differential strain and the triggered internal stress portions exists only in the direct vicinity of the bore hole, the strain gages grouped around the bore hole must be relatively small. Therefore such strain gage rosettes often have only diameters of approximately 10 to 15 mm, so that already small eccentricities can cause relatively large measuring errors. Therefore, the required maximum acceptable eccentricities of 0.02 mm often cannot be realized even with the above described very complicated boring apparatus.
Therefore, it is the underlying object of the invention to improve a measuring method and a strain gage rosette used therefor, for the internal stress measurement of workpieces according to the bore hole method in such a manner so that therewith very high measuring accuracies are achievable and this is realizable with the smallest possible measurement technology cost or effort.
This object is achieved by the invention set forth in the patent claims 1 and 10. Further developments and advantageous example embodiments of the invention are set forth in the dependent claims.
The invention has the advantage that the measuring errors due to small eccentricities can largely be compensated through the radially oppositely arranged measuring grids of a common measuring direction. For that, simply the measuring signals of the oppositely lying measuring grid pairs must be determined, whereby the measuring error due to the eccentricity of the bore hole can advantageously be improved by a factor of up to 20.
The invention further has the advantage that in such a rosette with two oppositely lying measuring grids of a measuring direction, the average value thereof can be achieved with the aid of a simple series or parallel circuit or simple arithmetic means, so that no significant measurement technological or equipment expenditure or effort is necessary for this.
The invention additionally has the advantage that simply through a doubling of the measuring grids on an otherwise similar strain gage rosette, the measuring accuracy can be improved by a multiple in a simple manner, without needing to have increased the effort or expense for the central introduction of the bore hole. In that regard, the additional effort or expanse for doubling the measuring grids on an otherwise similar rosette arrangement is relatively small, because the measuring grids are completely automatically produced through a common etching process on an otherwise similar carrier film or foil. Therefore, with such strain gage rosettes produced in an economical manner an increase of the measuring accuracy is advantageously to be achieved, even though the effort or expense of the centering accuracy can be reduced.

The invention is explained more closely in connection with an example embodiment, which is illustrated in the drawing. It is shown by:

FIG. 1 a six measuring grid bore hole rosette;

FIG. 2 a circuit foil for a six measuring grid bore hole rosette; and

FIG. 3 an eight measuring grid bore hole rosette.

FIG. 1 of the drawing shows a strain gage rosette 1 as a bore hole rosette, in which three similar or same- type measuring grids 3, 4, 5 are arranged at an angular spacing of 45° at a uniform radial spacing about a bore hole centering 2, and an allocated similar or same- type measuring grid 6, 7, 8 lies respectively opposite the measuring grids 3, 4, 5 symmetrically to the bore hole centering 2.
In that regard, the strain gage rosette 1 consists of a plastic carrier layer 9 on which six conventional meander- shaped measuring grids 3, 4, 5, 6, 7, 8 are applied. All measuring grids 3, 4, 5, 6, 7, 8 are thereby arranged concentrically about a central bore hole marking 2. Thereby the three left- 3, 4, 5, or right- side 6, 7, 8 measuring grids are provided like typical three grid bore hole rosettes about a bore hole marking 2, whereby all measuring grids 3, 4, 5, 6, 7, 8 comprise a common radial spacing to the bore hole marking 2. The three left-side measuring grids 3, 4, 5 are thereby oriented in three different directions between 0 to 90°. Between the measuring grids 3, 4, 5, a common angle of 45° is provided, so that the three left-side measuring grids 3, 4, 5 cover an angular range of 90°.
Internal stresses in workpieces or structural components can arise through internal or external forces that act on the workpiece. The form changes caused by the forces are characterized by longitudinal and crosswise displacements. The three tensions or stresses referenced to the unit area correspond to the internal forces in the workpiece. The stress conditions can be characterized on one, two or three axes, whereby the deformation conditions are always characterized on three axes. Therefore it is necessary, as long as the main strain directions are not known, to provide three measuring grids 3, 4, 5 oriented in different directions, in order to detect the deformation conditions. Because a conclusion of the internal stress can be determined computationally from the detected strain changes, basically the respective orientation of the measuring grids 3, 4, 5 is insignificant or unimportant, so that arrangements of 0°, 90° and 135°, or 0°, 60° and 120° also occur. Nonetheless, however, the three measuring grids 3, 4, 5 must always be oriented in different direction, so that an angular offset of 180° between two measuring grids 3, 4, 5 of a rosette was previously not known in bore hole rosettes.
For the special case, that for example the internal stress in one is of the main stress directions is known, then the internal stress measurement could, as an exception, also be detected with only two measuring grids oriented in deviating directions about a bore hole. This is not relevant practically, however, so that previous bore hole rosettes comprise at least three measuring grids, of which the angular spacings are always <180°. Therefore, with the illustrated six measuring grid bore hole rosette 1, the strains are detected in the three main strain directions of 0°, of 45° and 90°. This is achieved similarly by the three left-side measuring grids 3, 4, 5 as well as by the three right-side measuring grids 6, 7, 8, which lie opposite one another in a mirror symmetrical manner, and thus comprise a same spacing distance to the bore hole center point and the allocated opposite-lying measuring grids. Because all six measuring grids 3, 4, 5, 6, 7, 8 are embodied similarly, the measuring grid pairs 3, 8; 4, 7; 5, 6 respectively lying 180° opposite one another would basically have to detect the same strain during the boring process, because they are oriented in the same main strain direction.
The invention now uses this fact in order to correct unavoidable bore hole tolerances and therewith measuring inaccuracies due to an eccentric bore hole arrangement. Namely, with the presently demanded measuring accuracies, partially only maximum permissible eccentricities of 0.02 mm are tolerable, which are achievable with conventional bore hole centering methods only with great measurement technological effort and expanse. Due to the influence on the internal stresses to be detected, mechanical bore hole centerings, such as center punching and the like, are not permitted, so that in practice generally only eccentricities of >0.02 mm are achievable.
Therefore the invention suggests to provide two similar or same- type measuring grids 3, 8; 4, 7; 5, 6 lying 180° opposite one another on a strain gage rosette for at least each main strain direction to be detected, whereby the deviation of the measuring grids due to the eccentricity of the bore hole is substantially compensatable by an average value formation. For that it is then necessary, however, to average the detected strain measurement values of a main strain direction in order to minimize the error caused thereby. This is, however, not completely successful, because the calculable internal stresses do not run proportional to the spacing distance of the bore hole, so that a residual error remains. However, practical tests have resulted in an improvement of the measuring accuracy by the factor 20, for a highest possible eccentricity accuracy of, for example 0.02 mm. With a reduction of the effort or expense, with a simple bore hole centering method, eccentricities of for example 0.1 mm were still achievable, which still resulted in an improvement of the measuring accuracy by the factor 8 with the inventive bore hole rosette 1, compared to the highest possible maximum permissible eccentricity of a simple bore hole rosette with only three comparable measuring grids.
The invention proposes three different methods for the corresponding average value formation of the two measuring grid pairs 3, 8; 4, 7; 5, 6 that are arranged lying 180° opposite one another. Preferably the average value formation can be achieved by a series circuit connection of the respective opposite-lying and allocated two measuring grids 3, 8; 4, 7; 5, 6. Such a separate circuit foil 18 is shown in FIG. 2 of the drawing. In that regard, the circuit foil 18 is connected via copper wires 12, for example, with one another with the connection conductor paths 10 of the strain gage rosette guided out to the connection points 11. Thereby the circuit foil 18 already includes hard-wired conductor paths bridges 13, through which the measuring grid pairs 3, 8; 4, 7; 5, 6 of a main strain direction, which are arranged lying 180° opposite one another, are circuit-connected in series. Then on the output side, only six measurement conductor points 14 are still present, like in a conventional bore hole rosette with three measuring grids.
However, the six measuring grids 3, 4, 5, 6, 7, 8 can also be circuit-connected in series in a conventional manner by means of the twelve connection points 11 of the six measuring grid bore hole rosette 1, in order to obtain the average value of a strain direction respectively as output signals.
Such a fixed circuit-connection could, however, be provided directly on the carrier film 9 of the bore hole rosette 1. Because the conductor paths 10 would, however, cross one another thereby, this is only possible through a bore hole rosette 1 with a stacked construction.
An average value formation could, however, also be achieved through a parallel circuit of the allocated measuring grid pairs 3, 8; 4, 7; 5, 6 of a strain direction, which are arranged lying 180° opposite one another. Because the measurement signals of each measuring grid 3, 4, 5, 6, 7, 8 are often still supplied to an analog-digital converter after the amplification, this could also be carried out subsequently in a computational manner by means of a simple computer circuit. Then for that purpose, in connection with larger eccentricities, correction factors could still be provided, which compensates the non-linearity to the bore hole deviation.
A further embodiment of a strain gage rosette is shown in FIG. 3 of the drawing as an eight measuring grid bore hole rosette 15. This differs from the six measuring grid bore hole rosette 1 simply by a further pair of similar or same- type measuring grids 16, 17, with which an additional strain direction of a material can be detected. In that regard, the additional measuring grid pair 16, 17 is arranged in an angular spacing of 45° to the neighboring measuring grid pairs. Thereby an improvement of the accuracy is preferably achieved in connection with an eccentricity that would have extended in the grid-free direction in a six measuring grid bore hole rosette 1. Furthermore, the measuring accuracy is already increased due to the increase of the evaluatable measurement signals, especially if the main strain direction extends in the direction that was previously not provided with a measuring grid. Moreover, bore hole rosettes with further measuring grid pairs can still also be embodied, in so far as the space conditions on the carrier layer 9 allow this for the measuring grids arranged close to the bore hole. Namely, in the above described example embodiment, the two bore hole rosettes 1, 15 have only a diameter or an edge length of preferably 12 mm. Therefore, an increase of the number of measuring grids over eight is preferably only presented for larger bore hole diameters. Namely, in the bore hole method, the bore hole diameter and its bore hole depth is primarily determined according to the analysis depth, so that not always only small bore hole diameters are sufficient.

Claims

1 to 10. (canceled)

11. A strain gage rosette arrangement for stress measurement on a workpiece, comprising:

a common carrier film arrangement, comprising a carrier film;

a centering mark provided on said carrier film arrangement;

a total of exactly eight strain gage measuring grids arranged on said common carrier film arrangement respectively on eight radial lines extending radially outwardly from said centering mark, wherein said radial lines are successively spaced radially from on another by 45° about said centering mark, and wherein said eight strain gage measuring grids form four opposite pairs of respectively two of said measuring grids that respectively lie 180° opposite one another about said centering mark; and

a circuit arrangement by which said two measuring grids of each one of said opposite pairs respectively are circuit-connected or coupled with one another such that respective output values of said two measuring grids of each said opposite pair will be averaged with one another.

12. The strain gage rosette arrangement according to claim 11, wherein said two measuring grids of each one of said opposite pairs respectively are positioned with the same nominal radial spacing distance relative to said centering mark.

13. The strain gage rosette arrangement according to claim 11, wherein said centering mark is a bore hole mark.

14. The strain gage rosette arrangement according to claim 11, wherein said circuit arrangement includes two connection points or soldering points respectively at terminal ends of two conductor leads connected to each respective one of said measuring grids, for a total of sixteen of said connection points or soldering points on sixteen of said conductor leads.

15. The strain gage rosette arrangement according to claim 14, wherein said conductor leads are arranged on said carrier film arrangement, and said connection points or soldering points are all arranged along a longitudinal side of said carrier film arrangement.

16. The strain gage rosette arrangement according to claim 14, wherein said circuit arrangement further includes connection conductor paths which connect together in series or in parallel said connection points or soldering points that are respectively connected to said two respective measuring grids of each one of said opposite pairs of said measuring grids.

17. The strain gage rosette arrangement according to claim 16, wherein said two measuring grids of each respective one of said opposite pairs are connected together in series with one another via said conductor leads and said connection conductor paths.

18. The strain gage rosette arrangement according to claim 16, wherein said two measuring grids of each respective one of said opposite pairs are connected together in parallel with one another via said conductor leads and said connection conductor paths.

19. The strain gage rosette arrangement according to claim 16, wherein said connection conductor paths are arranged on said common carrier film arrangement.

20. The strain gage rosette arrangement according to claim 16, further comprising a separate carrier film that is separate from said common carrier film arrangement, wherein said connection conductor paths are arranged on said separate carrier film.

21. The strain gage rosette arrangement according to claim 16, wherein said connection conductor paths are conductive paths of a circuit foil.

22. The strain gage rosette arrangement according to claim 11, wherein said circuit arrangement respectively connects together in series with one another said two measuring grids of each respective one of said opposite pairs of said measuring grids.

23. The strain gage rosette arrangement according to claim 11, wherein said circuit arrangement respectively connects together in parallel with one another said two measuring grids of each respective one of said opposite pairs of said measuring grids.

24. The strain gage rosette arrangement according to claim 11, wherein said circuit arrangement comprises conductor path bridges that are stacked and cross one another.

25. The strain gage rosette arrangement according to claim 11, wherein said circuit arrangement includes a total of eight external connection points, wherein respective pairs of said external connection points connect to said respective opposite pairs of said measuring grids.

26. The strain gage rosette arrangement according to claim 11, wherein said radial lines are identified by radial line markings on said carrier film arrangement.

27. The strain gage rosette arrangement according to claim 11, wherein said radial lines are virtual figurative lines.

28. A strain gage rosette arrangement for stress measurement on a workpiece, comprising:

a common carrier film arrangement comprising a carrier film;

a centering mark provided on said carrier film arrangement;

at least six strain gage measuring grids arranged on said common carrier film arrangement respectively on at least six radial lines extending radially outwardly from said centering mark, wherein said radial lines are successively spaced radially from one another about said centering mark, opposite pairs of said radial lines are arranged 180° opposite one another about said centering mark, and opposite pairs of respectively two of said measuring grids respectively lie on said opposite pairs of said radial lines 180° opposite one another about said centering mark;

two conductor leads respectively for each one of said measuring grids, wherein said conductor leads are all arranged on said common carrier film arrangement, and wherein said conductor leads respectively terminate at respective connection points, such that a total number of said connection points is twice a total number of said measuring grids; and

a circuit foil that includes conductor paths which are connected to said connection points of said conductor leads so as to respectively connect together in series or in parallel said two respective measuring grids of each respective one of said opposite pairs of said measuring grids, wherein said conductor paths of said circuit foil respectively terminate at respective measurement output points, such that a total number of measurement output points is equal to a total number of said measuring grids.

29. The strain gage rosette arrangement according to claim 28, wherein said total number of said measuring grids is exactly six.

30. The strain gage rosette arrangement according to claim 28, wherein said total number of said measuring grids is exactly eight.

31. The strain gage rosette arrangement according to claim 28, wherein said circuit foil is separate from said common carrier foil arrangement.